Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle


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Abstract

To calculate the durability of gas turbine engine parts damaged by low-cycle fatigue (LCF), according to the “Structural codes of turbine engine strength” it is necessary to test specimens cut from respective parts (or test coupons) under “hard” loading. “Hard” here means there is a fixed strain cycle. The tests are conducted with different asymmetry coefficients of the strain cycle and with different exposure time at the maximum cycle strain (to take into account the effect of creep at high temperatures). The tests carried out are to provide sufficient statistics to ensure the reliability of the calculation. We suggest a method of assessing the durability of gas turbine engine parts based on testing standard specimens at zero-to-“soft loading” cycle using modified Manson-Coffin’s equation. The results of the work confirm the possibility of achieving the required adequacy of assessing the durability of parts damaged by the LCF mechanism with the use of a modified Manson-Coffin equation. Some recommendations concerning its application are given.

About the authors

V. F. Pavlov

Samara National Research University

Author for correspondence.
Email: sopromat@ssau.ru

Doctor of Science (Engineering), Professor

Head of the Department of Strength of Materials

Russian Federation

V. A. Kirpichyov

Samara National Research University

Email: dean_fla@ssau.ru

Doctor of Science (Engineering)

Professor of the Department of Strength of Materials

Russian Federation

E. E. Kocherova

Samara National Research University

Email: kocherova_2020@mail.ru

Postgraduate student of the Department of Strength of Materials

Russian Federation

A. S. Zlobin

Samara National Research University

Email: as.zlobin@mail.ru

Postgraduate student of the Department of Strength of Materials

Russian Federation

References

  1. Normy prochnosti aviatsionnykh gazoturbinnykh dvigateley grazhdanskoy aviatsii [Strength standards of aviation gas turbine engines of civil aviation]. Moscow: CIAM Publ., 2004. 260 p. (In Russ.)
  2. Teren’t’ev V.F, Petukhov A.N. Ustalost’ vysokoprochnykh metalicheskikh materialov [Fatigue of high-strength metallic materials]. Moscow: CIAM Publ., 2013. 515 p.
  3. Parton V.Z., Borisovskiy V.G. Dinamika khrupkogo razrusheniya [Dynamics of brittle fracture]. Moscow: Mashinostroenie Publ., 1988. 240 p.
  4. Anurov U.M., Fedorchenko D.G. Osnovy obespecheniya prochnostnoy nadezhnosti aviatsionnykh dvigateley i silovykh ustanovok [The principles of ensuring the strength reliability of aircraft engines and power units]. St.-Peterburg: Peter the Great Saint-Petersburg Polytechnic University Publ., 2004. 390 p.
  5. Kudryavtsev I.V., Naumchenko N.E., Savvina N.M. Ustalost' krupnykh detaley mashin [Fatigue of large machine parts]. Moscow: Mashinostroenie Publ., 1981. 240 p.
  6. Kolmogorov V.L. Napryazheniya, deformatsii, razrushenie [Stresses, deformations, destruction]. Moscow: Metallurgiya Publ., 1970. 229 p.
  7. Kudryavtsev P.I. Nerasprostranyayushchiesya ustalostnye treshchiny [Non-propagating fatigue cracks]. Moscow: Mashinostroenie Publ., 1982. 174 p.
  8. GOST 25.502-79. Strength analysis and testing in machine building. Methods of metals mechanical testing. Methods of fatigue testing. Moscow: Standartinform Publ., 1983. 50 p. (In Russ.)
  9. Makhutov N.A., Gadenin M.M., Burak M.I, Daunis M.A., Zatsarini V.V., Zlochevsky A.B., Kagan V.A., Larionov V.V., Levin O.A., Novikov V.A., Pokrovsky V.V., Romanov A.N., Troschenko V.T., Filatov V.M. Mekhanika malotsiklovogo razrusheniya [Mechanics of Low-Cicle Fracture]. Moscow: Nauka Publ., 1986. 264 p.
  10. Makhutov N.A. Deformatsionnye kriterii razrusheniya i raschet elementov konstruktsiy na prochnost' [Deformation fracture criteria and strength calculation of structural components]. Moscow: Mashinostroenie Publ., 1981. 272 p.

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